Method of Matching Sensors in a Multi-Probe Turbine Blade Vibration Monitor

• US 20090078052A1
• Filed: 10/25/2007
• Published: 03/26/2009
• Est. Priority Date: 09/21/2007
• Status: Active Grant

• Current Assignee: Siemens Energy Incorporated (Siemens AG)
• Original Assignee: Siemens Power Generation, Inc.
• Inventors: Twerdochlib, Michael
• Granted Patent: US 7,987,725 B2
• Time in Patent Office: Days
• US Class Current: 73/660
• CPC Class Codes: G01H 1/003 of rotating machines G01H1/10 takes precedence
• CPC Class Codes: G01H 1/08 Amplitude

Abstract

A method of matching sensors in a multi-probe blade vibration monitor for a turbine. The method includes providing at least two probes mounted in a casing of the turbine adjacent to a rotating blade structure of the turbine. Targets are provided on radially outer portions of the blade structure. Each of the probes includes a sensor generating signals corresponding to target passing events, and a set of synchronous harmonics of the rotational speed of the rotor are produced for each sensor. The position of the sensors is adjusted such that the sets of harmonics of the sensors are substantially matched, indicating that the positions of the sensors are matched.

Claims

1. A method of matching sensors in a multi-probe blade vibration monitor for a turbine, said turbine comprising a plurality of radially extending blades mounted on a rotor for rotation about a rotational axis, said blade structure including a plurality of targets located at radially outer locations of said blade structure, the method comprising:

providing at least two probes mounted in a casing of said turbine adjacent to said blade structure, each of said probes including a sensor;

generating signals from each of said sensors corresponding to target passing events when each said target passes said sensors;

analyzing said signals to create, for each said sensor, a set of harmonics characteristic of the position of each of said sensors relative to said plurality of targets; and

comparing said sets of harmonics for at least two of said sensors, and positioning said sensors such that, for at least two of said sensors, said sets of harmonics are substantially matched, indicating that said at least two sensors are at matched axial locations relative to said plurality of targets.

2. The method of claim 1, wherein said harmonics comprise synchronous harmonics of the rotational speed of said rotor.

3. The method of claim 1, wherein said step of positioning said sensors comprises moving at least one of said sensors about a rotational axis of a respective probe.

4. The method of claim 3, wherein said at least one sensor is translated in an axial direction parallel to said rotational axis of said rotor during said movement about said rotational axis of said respective probe.

5. The method of claim 1, wherein said step of comparing said sets of harmonics comprises comparing preselected harmonics that are sensitive to the position of said sensors relative to said targets.

6. The method of claim 5, wherein said harmonics comprise synchronous harmonics of the rotational speed of said rotor.

7. The method of claim 1, wherein said step of comparing said sets of harmonics comprises forming a plot of each said set of harmonics, each said plot defining a fingerprint corresponding to the position of a respective sensor.

8. The method of claim 7, wherein said sets of harmonics comprise selected subsets of synchronous harmonics of the rotational speed of said rotor.

9. A method of matching sensors in a multi-probe blade vibration monitor for a turbine, said turbine comprising a plurality of radially extending blades mounted on a rotor for rotation about a rotational axis, said blade structure including a plurality of targets located at radially outer locations of said blade structure, the method comprising:

providing at least two probes mounted in a casing of said turbine adjacent to said blade structure, each of said probes including a sensor;

generating signals from each of said sensors corresponding to target passing events when each said target passes said sensors;

analyzing said signals to create, for each said sensor, a set of synchronous harmonics of the rotational speed of said rotor; and

positioning said sensors such that, for at least two of said sensors, said sets of harmonics are substantially matched, indicating that said at least two sensors are at matched axial locations relative to said plurality of targets.

10. The method of claim 9, wherein said step of positioning said sensors comprises moving at least one of said sensors about a rotational axis of a respective probe.

11. The method of claim 10, wherein said sensors are mounted eccentrically relative to respective rotational axes of said probes.

12. The method of claim 11, wherein said at least one sensor is translated in an axial direction parallel to said rotational axis of said rotor during said movement about said rotational axis of said respective probe.

13. The method of claim 10, wherein said step of positioning said sensors further comprises comparing a first set of harmonics from said at least one sensor to a second set of harmonics from another of said sensors and rotating said at least one sensor about said rotational axis of said probe such that said first set of harmonics substantially matches said second set of harmonics.

14. The method of claim 13, wherein said step of comparing said sets of harmonics comprises forming a plot of each said set of harmonics, each said plot defining a fingerprint corresponding to the position of a respective sensor.

15. The method of claim 14, wherein said sets of harmonics comprise selected subsets of said synchronous harmonics of the rotational speed of said rotor.